Attenuation in a Shock Tube due to Unsteady-Boundary-Layer Action. Mirels, H. Technical Report 1333, National Advisory Committee for Aeronautics, 1957.
bibtex   
@techreport{mirels1957,
	title = {Attenuation in a {Shock} {Tube} due to {Unsteady}-{Boundary}-{Layer} {Action}},
	number = {1333},
	institution = {National Advisory Committee for Aeronautics},
	author = {Mirels, Harold},
	year = {1957},
}

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